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The pilot was conducting a survey flight for the Park and Wildlife Commission during which time his passengers would inspect fire plots. He located an area near to one fire plot which he considered suitable for a landing. It was a small oval shaped clearing in a valley 420ft above mean sea level, approximately 30ft x 50ft in size, surrounded by trees 30 to 50ft in height, with smaller trees scattered in the clearing. The pilot reported that he was not conscious of any wind, and made a steep approach to the south east over the lower trees. Before landing he hovered the helicopter to check the clearance of his tail rotor with the small trees, and then commenced to set it down in the long grass. He noticed that the area had a substantial sideways slope so he brought the helicopter back into the hover to find a more suitable landing area in the clearing. Being unable to find a level area he decided to take-off and look for another clearing. After completing the pre-takeoff checks in the hover, and ascertaining the available engine power, he made a vertical ascent, facing into the south east, and climbed to approximately 40ft above ground level, being about 10ft above the tree tops in this direction. As he initiated forward flight the helicopter began to sink and loose main rotor RPM, which he was unable to regain in the time available by lowering the collective control to reduce the main rotor blade pitch angle. He turned the helicopter through 90 degrees to the right, which would have reduced the tail rotor blade pitch angle, but it kept on descending without any rotor RPM increase. He then turned left and tried to find enough room through the trees to afford a recovery, but the main rotor struck a tree about 20ft above ground level and the helicopter rolled to the right before impacting the ground. The pilot and his two passengers evacuated with minor injuries. The helicopter was 73kg below its maximum take-off weight at departure, and within its longitudinal and lateral balance limits. The temperature was about 28 degrees Celsius and a very high humidity, with the density altitude approximately 2,000ft. In these conditions the helicopter?s performance would have been reduced, but it still had sufficient engine power at take-off to effect a vertical climb, which would have reached its limit when the helicopter was hovering out of ground effect at the top of the climb.. As he changed from the hover to forward flight, the pilot probably increased collective pitch slightly to overcome a loss of height as the cyclic control was moved forward. This would have started the rotor RPM decay as no more engine power was available to maintain it. There was insufficient height above the tree tops for the helicopter to settle and allow time for the rotor RPM to recover when the collective control was reduced, or to obtain airspeed by diving to provide translational lift. The pilot reported a nil wind condition, but thought he may have experienced a slight tailwind during the climb. In either condition, with the engine power available, he would have had difficulty hovering out of ground effect, then initiating forward flight without some form of translational lift being available, such as a headwind or by diving.
Download Final Report
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General details
Date: 14 January 1997 Investigation status: Completed 
Time: 10:30 CST Investigation type: Occurrence Investigation 
 Occurrence type:Collision with terrain 
 Occurrence class: Operational 
Release date: 20 January 1997 Occurrence category: Accident 
Report status: Final  
 
Aircraft details
Aircraft manufacturer: Kawasaki Heavy Industries 
Aircraft model: 47G3B-KH4 
Aircraft registration: VH-KIO 
Sector: Helicopter 
Damage to aircraft: Substantial 
Departure point:Katherine River Gorge NT
Destination:Katherine River Gorge NT
 
 
 
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Last update 28 October 2014